Description:
The J-2X is a 294,000-pound of thrust rocket engine based on the J-2 and J-2S engines from Apollo-Saturn space vehicle program. It has been selected to power the upper stages of Ares I and Ares V space launch vehicles which are meant to transport humans to the Moon and beyond. NASA awarded a $1.2 billion development contract to Pratt & Whitney Rocketdyne on July 18, 2007. The contract funds design, development and test of the J-2X rocket motor including both ground and flight tests through December 31, 2012.
Specifications Engine/s Performance: Thrust 294,000 lb (133,358 kg)
Applications
Ares I, Ares V
J-2X - Contracts, Orders & Sales
News
Operators
United States of America / Planned
Notes (*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)